Active Control of Fan-Generated Tone Noise-Reference-Cited by-同舟云学术

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Active Control of Fan-Generated Tone Noise

Published:1997-01 Issue:1 Volume:35 Page:17-22
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gerhold Carl H.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.81

Reference16 articles.

1. Dungan, M. E. “ Development of a Compact Sound Source for the Active Control of Turbofan Inlet Noise,” M.S. Thesis, Mechanical Engineering Dept., Virginia Polytechnic Inst.and State Univ., Blacksburg, VA,June 1992.

2. The active control of sound propagation in long ducts

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1. Analysis of liner performance using the NASA Langley Research Center Curved Duct Test Rig;Applied Acoustics;2016-01

2. Modal Feedback Control of Flexible Structures;Advances in Industrial Control;2010

3. Experimental validation of tonal noise control from subsonic axial fans using flow control obstructions;Journal of Sound and Vibration;2009-03

4. Robust control of flexible structures with stable bandpass controllers;Automatica;2008-05

5. Investigation of Liner Characteristics in the NASA Langley Curved Duct Test Rig;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21

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